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Um OALOHM... ntiltiatune gut nw.<br />

You can depend on 4<br />

TYPE RH<br />

MINIATURE POWER RESISTORS<br />

For all applications where the equipment must survive<br />

the most severe environmental, shock, vibration, humidity<br />

and temperature conditions.<br />

Smallest in size; completely welded from terminal to<br />

terminal; silicone sealed in a die -cast black anodized<br />

aluminum housing and mounts on sub -panel for maximum<br />

heat dissipation; impervious to moisture, salt<br />

ions, vapor and gases.<br />

Three wattage ranges: RH -25, 25 watts;<br />

RH -50, 50 watts; RH -250, 250 watts.<br />

Temperature coefficient 0.00002 /Deg. C<br />

Ranges from 0.1 ohm to 55,000 ohms,<br />

depending on type<br />

Tolerances 0.05 %, 0.1 %, 0.25 %,<br />

0.5 %, 1 %, 3 %, 5%<br />

Conform to applicable JAN and MIL Specifications<br />

Write for Bulletin R -21 -6<br />

DALE PRODUCTS, INC_<br />

Phone 2139<br />

1304 28th Ave. Columbus, Nebraska, U.S.A.<br />

<strong>TELE</strong>METRY<br />

E<br />

At RREP, systems engineering<br />

assumes paramount importance.<br />

<strong>Com</strong>ponent and assembly design<br />

are examined critically, always<br />

in relationship to the overall<br />

system. And unique building<br />

block design permits individual<br />

components and assemblies to<br />

be package engineered into form<br />

iU<br />

Export Dept t<br />

Pan -Mar Corp.,<br />

1270 Broadway<br />

New York 1, N.<br />

In Canada:<br />

Charles W. Pointen, Ltd.<br />

6 Alcin° Ave., Toronto<br />

SYSTEMS<br />

WI HETHIE G<br />

CREATIVE<br />

SPARK<br />

factors to fulfill a wide variety<br />

of applications.<br />

It is no accident that U. S. military<br />

agencies, foreign governments,<br />

most aircraft companies<br />

and many research and industrial<br />

organizations specify RREP<br />

telemetric data transmitting systems<br />

for reliability under extreme<br />

operating conditions.<br />

CREATIVE ENGINEERING IS THE DIFFERENCE!<br />

Technical bulletins describing RREP's complete line<br />

of telemetering equipment available upon request.<br />

RREP Type 1001A Crystal Controlled Transmitter.<br />

RF power output: 3.5 to 4.5 watts into<br />

52 -ohm load. Frequency range: 215 to 235 megacycles.<br />

Frequency stability: ±0.005 %.<br />

1111E15<br />

RAYMOND ROSEN<br />

ENGINEERING PRODUCTS, INC.<br />

32nd & Walnut Streets, Philadelphia 4, Pennsylvania<br />

15106 Ventura Boulevard, Sherman Oaks, California<br />

Finned Magnetron<br />

(Continued from page 174)<br />

were built and tested. The dummy<br />

magnetron used for the tests with<br />

the various cooling fins employed<br />

a coiled nichrome wire heater,<br />

housed within a simulated anode<br />

block, and a r -f output pipe connected<br />

to the simulated anode block<br />

(see Fig. 2). The test equipment<br />

consisted of a positive displacement<br />

blower supplying air, metered by a<br />

rotameter, to a plenum chamber;<br />

the air passed from the plenum<br />

chamber through a transition piece<br />

into the magnetron.<br />

For each set of cooling fins, temperature<br />

and pressure drop characteristics<br />

were obtained over a<br />

range of airflows. In all cases fin<br />

thickness was .030 in., with .080 in.<br />

between fins; overall fin length and<br />

width were approximately 3 x 31/2<br />

in. for all fins except the original<br />

fin (Fig. 3) which was approximately<br />

21/2 in. sq. Inlet air temperature<br />

was 30 °C. The location of<br />

the hot spot temperature tx,,,,px is<br />

shown in Fig. 2.<br />

A typical curve of (tc,n,ax tt,Inlet)<br />

and pressure drop as a function of<br />

airflow is given in Fig. 4 for the<br />

set of original fins (Fig. 3). All 4<br />

types of fin modifications, shown in<br />

Figs. 5, 6 and 7, gave substantial<br />

improvements over this original design.<br />

Fig. 5 shows the first modification,<br />

a fin with deflector vanes. The<br />

purpose of the vanes was to force<br />

more air to flow over the output<br />

pipe, since the pipe temperature is<br />

close to the anode temperature and<br />

the pipe conducts much of the heat<br />

away from the anode. It was<br />

thought this would cause an increase<br />

in local h at this region for<br />

any given flow, and therefore demand<br />

less air to achieve the overall<br />

hS product required. The dummy<br />

magnetron with a set of this type<br />

of fins required only 29 cfm and 2.8<br />

in. of water to have a satisfactory<br />

hS value.<br />

An improvement over the fin of<br />

Fig. 5 was considered possible by<br />

deflecting all of the air more<br />

gradually over the outlet pipe,<br />

thereby increasing h locally, and<br />

reducing the loss associated with<br />

the turning. This could be ac-<br />

(Continued on page 178)<br />

176 For product information, use inquiry cord on pages 209 -210 Tele -Tech & ELECTRONIC INDUSTRIES June 1956

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